It is an ultra-light, single-seat, conventional helicopter, powered by a Rotax engine. Its develop emerged from the need for an aircraft capable of being used for evaluating different solutions in flight, as well as systems to be used in the CH-5. This turned out to be an aircraft with excellent maneuvering and stability. The main frame is made of steel tubes and the blades are made of composite materials. The command system is unique and it has been patented by Augusto Cicaré. First flight: 1987

Overview

Data on design, manufacture and status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Other

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 1.60 m (5.2 ft)

Overall Length: 7.15 m (23.5 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Rotax Rotax 582 reciprocating

Engine manufacturer: BRP-Powertrain GmbH & Co KG

Max continuous power: 65 kW (87 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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Related Public Resources

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